Fuel nozzles

Abstract

A nozzle includes a nozzle body defining a longitudinal axis. The nozzle body has an air passage, a fuel circuit radially outboard from the air passage with respect to the longitudinal axis, and a cooling circuit. The fuel circuit extends from a fuel circuit inlet to a fuel circuit annular outlet. The fuel circuit is defined between a fuel circuit inner wall and a fuel circuit outer wall. At least a portion of the fuel circuit outer wall is radially outboard from the fuel circuit inner wall with respect to the longitudinal axis. A cooling circuit is defined within at least one of the fuel circuit inner wall or the fuel circuit outer wall. The cooling circuit extends from an axial position proximate the fuel circuit inlet to an axial position proximate the fuel circuit outlet.

What is claimed is: 
     
       1. A nozzle, comprising:
 a nozzle body defining a longitudinal axis including:
 an air passage; 
 a fuel circuit radially outboard from the air passage with respect to the longitudinal axis, the fuel circuit extending from a fuel circuit inlet to a fuel circuit annular outlet, wherein the fuel circuit is defined between a fuel circuit inner wall and a fuel circuit outer wall, wherein at least a portion of the fuel circuit outer wall is radially outboard from the fuel circuit inner wall with respect to the longitudinal axis; and 
 a cooling circuit defined within at least one of the fuel circuit inner wall and the fuel circuit outer wall, wherein the cooling circuit extends from a first axial position proximate the fuel circuit inlet to a second axial position proximate the fuel circuit outlet; and 
 
 a stem operatively connected to a fuel manifold of the nozzle body, wherein the stem includes three liquid channels for fluid communication with at least one of the fuel circuit or the cooling circuit, wherein one of the three liquid channels is a coolant-in channel in fluid communication with a distribution channel of the cooling circuit to provide coolant thereto, wherein one of the three liquid channels is a coolant-out channel in fluid communication with a collection channel of the cooling circuit to receive coolant therefrom, wherein the distribution channel and the collection channel are circumferentially spaced apart from one another. 
 
     
     
       2. The nozzle as recited in  claim 1 , further wherein one of the three liquid channels is a fuel channel in fluid communication with the fuel manifold to provide fuel to the fuel circuit inlet. 
     
     
       3. The nozzle as recited in  claim 1 , wherein the distribution channel and the collection channel are co-planar. 
     
     
       4. The nozzle as recited in  claim 1 , wherein the cooling circuit includes a pair of helical threads, wherein a first one of the helical threads begins at the distribution channel and extends to the second axial position proximate the fuel circuit outlet to provide cooling flow to a nozzle tip, and wherein a first end of a second one of the helical threads is connected to the first one of the helical threads proximate to the fuel circuit outlet and extends to the collection channel to provide a cooling flow exit to the coolant-out channel. 
     
     
       5. The nozzle as recited in  claim 4 , wherein the first end of the second one of the helical threads is connected to the first one of the helical threads through a short circuit segment. 
     
     
       6. The nozzle as recited in  claim 1 , wherein the nozzle body includes a pair of tubes defined through the air passage and though theft fuel manifold, wherein one of the tubes fluidly connects the distribution channel to the coolant-in channel and another one of the tubes fluidly connects the collection channel to the coolant-out channel. 
     
     
       7. The nozzle as recited in  claim 6 , wherein the air passage includes an annular inlet having radial swirl vanes circumferentially spaced apart from one another, wherein the tubes are defined within the radial swirl vanes. 
     
     
       8. The nozzle as recited in  claim 1 , wherein the air passage is defined between a backing plate and a jacket downstream from the backing plate, wherein at least a portion of the jacket is a conical shape that converges toward the longitudinal axis in a downstream direction. 
     
     
       9. The nozzle as recited in  claim 1 , wherein the air passage includes a radial swirler, a converging conical cross-section, and an annular inlet, wherein the radial swirler includes radial swirl vanes circumferentially spaced apart from one another about the annular inlet to induce swirl into air entering the annular inlet of the air passage. 
     
     
       10. The nozzle as recited in  claim 1 , wherein the nozzle body includes an outer air passage defined radially outboard of the fuel circuit with respect to the longitudinal axis. 
     
     
       11. The nozzle as recited in  claim 10 , wherein the outer air passage is defined between the fuel circuit outer wall and an outer air passage wall, and wherein the outer air passage is a converging non-swirling outer air passage. 
     
     
       12. A nozzle, comprising:
 a nozzle body defining a longitudinal axis including:
 an air passage, wherein the air passage includes a radial swirler, a converging conical cross-section, and an annular inlet, wherein the radial swirler includes radial swirl vanes circumferentially spaced apart from one another about the annular inlet to induce swirl into air entering the annular inlet of the air passage; 
 a fuel circuit radially outboard from the air passage with respect to the longitudinal axis, the fuel circuit extending from a fuel circuit inlet to a fuel circuit annular outlet, wherein the fuel circuit is defined between a fuel circuit inner wall and a fuel circuit outer wall, wherein at least a portion of the fuel circuit outer wall is radially outboard from the fuel circuit inner wall with respect to the longitudinal axis; and 
 a cooling circuit defined within at least one of the fuel circuit inner wall and the fuel circuit outer wall, wherein the cooling circuit extends from a first axial position proximate the fuel circuit inlet to a second axial position proximate the fuel circuit outlet; and 
 
 a stem operatively connected to a fuel manifold of the nozzle body, wherein the stem includes three liquid channels for fluid communication with at least one of the fuel circuit or the cooling circuit, wherein one of the three liquid channels is a coolant-in channel in fluid communication with a distribution channel of the cooling circuit to provide coolant thereto, wherein one of the three liquid channels is a coolant-out channel in fluid communication with a collection channel of the cooling circuit to receive coolant therefrom. 
 
     
     
       13. The nozzle as recited in  claim 12 , wherein one of the three liquid channels is a fuel channel in fluid communication with the fuel manifold to provide fuel to the fuel circuit inlet. 
     
     
       14. The nozzle as recited in  claim 12 , wherein the distribution channel and the collection channel are co-planar. 
     
     
       15. The nozzle as recited in  claim 12 , wherein the cooling circuit includes a pair of helical threads, wherein a first one of the helical threads begins at the distribution channel and extends to the second axial position proximate the fuel circuit outlet to provide cooling flow to a nozzle tip, and wherein a first end of a second one of the helical threads is connected to the first one of the helical threads proximate to the fuel circuit outlet and extends to the collection channel to provide a cooling flow exit to the coolant-out channel. 
     
     
       16. The nozzle as recited in  claim 15 , wherein the first end of the second one of the helical threads is connected to the first one of the helical threads through a short circuit segment. 
     
     
       17. The nozzle as recited in  claim 12 , wherein the nozzle body includes a pair of tubes defined through the air passage and though the fuel manifold, wherein one of the tubes fluidly connects the distribution channel to the coolant-in channel and another one of the tubes fluidly connects the collection channel to the coolant-out channel. 
     
     
       18. The nozzle as recited in  claim 17 , wherein the air passage includes an annular inlet having radial swirl vanes circumferentially spaced apart from one another, wherein the tubes are defined within the radial swirl vanes. 
     
     
       19. The nozzle as recited in  claim 12 , wherein the air passage is defined between a backing plate and a jacket downstream from the backing plate, wherein at least a portion of the jacket is a conical shape that converges toward the longitudinal axis in a downstream direction. 
     
     
       20. The nozzle as recited in  claim 12 , wherein the nozzle body includes an outer air passage defined radially outboard of the fuel circuit with respect to the longitudinal axis.